SCALING WAKE-PARTICLE INTERACTIONS FOR AERIAL APPLICATIONS RESEARCH.

Allen I. Ormsbee; Michael B. Bragg; Mark D. Maughmer

SCALING WAKE-PARTICLE INTERACTIONS FOR AERIAL APPLICATIONS RESEARCH.

Allen I. Ormsbee, Michael B. Bragg, Mark D. Maughmer

Aerospace Engineering

Research output: Contribution to journal › Conference article › peer-review

Abstract

The differential equation for the trajectory of a spherical particle injected into an aircraft wake was developed and the proper scaling relations extracted. After some simplification a convenient set of similarity parameters, a scale model test program was designed and performed in the NASA Langley vortex research facility. The results of the tests demonstrated the validity of the similarity parameters in conducting scale model testing for aerial application research.

Original language	English (US)
Journal	AIAA Paper
State	Published - 1980
Event	AIAA Pap AIAA Aircr Syst Meet - Anaheim, Calif Duration: Aug 4 1980 → Aug 6 1980

All Science Journal Classification (ASJC) codes

General Engineering

Cite this

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title = "SCALING WAKE-PARTICLE INTERACTIONS FOR AERIAL APPLICATIONS RESEARCH.",

abstract = "The differential equation for the trajectory of a spherical particle injected into an aircraft wake was developed and the proper scaling relations extracted. After some simplification a convenient set of similarity parameters, a scale model test program was designed and performed in the NASA Langley vortex research facility. The results of the tests demonstrated the validity of the similarity parameters in conducting scale model testing for aerial application research.",

author = "Ormsbee, {Allen I.} and Bragg, {Michael B.} and Maughmer, {Mark D.}",

year = "1980",

language = "English (US)",

journal = "AIAA Paper",

issn = "0146-3705",

}

TY - JOUR

T1 - SCALING WAKE-PARTICLE INTERACTIONS FOR AERIAL APPLICATIONS RESEARCH.

AU - Ormsbee, Allen I.

AU - Bragg, Michael B.

AU - Maughmer, Mark D.

PY - 1980

Y1 - 1980

N2 - The differential equation for the trajectory of a spherical particle injected into an aircraft wake was developed and the proper scaling relations extracted. After some simplification a convenient set of similarity parameters, a scale model test program was designed and performed in the NASA Langley vortex research facility. The results of the tests demonstrated the validity of the similarity parameters in conducting scale model testing for aerial application research.

AB - The differential equation for the trajectory of a spherical particle injected into an aircraft wake was developed and the proper scaling relations extracted. After some simplification a convenient set of similarity parameters, a scale model test program was designed and performed in the NASA Langley vortex research facility. The results of the tests demonstrated the validity of the similarity parameters in conducting scale model testing for aerial application research.

UR - http://www.scopus.com/inward/record.url?scp=85095893366&partnerID=8YFLogxK

UR - http://www.scopus.com/inward/citedby.url?scp=85095893366&partnerID=8YFLogxK

M3 - Conference article

AN - SCOPUS:85095893366

SN - 0146-3705

JO - AIAA Paper

JF - AIAA Paper

T2 - AIAA Pap AIAA Aircr Syst Meet

Y2 - 4 August 1980 through 6 August 1980

ER -

SCALING WAKE-PARTICLE INTERACTIONS FOR AERIAL APPLICATIONS RESEARCH.

Abstract

All Science Journal Classification (ASJC) codes

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